Tecnam P2006T - Page 164

Page 5 - 18
Section 5 - Performances
CRUISE PERFORMANCES
4
th
Edition, Rev. 0
Weight: 1150 kg
Pressure Altitude: 9000 ft
ISA – 30°C (-33°C)
ISA (-3°C)
ISA + 30°C (27°C)
RPM
*
MAP
PWR
KTAS
F.C.
**
PWR
KTAS
F.C.
**
PWR
KTAS
F.C.
**
[inHg]
[lt/hr]
[lt/hr]
[lt/hr]
2388
21.1
75%
137
20.9
71%
139
19.7
67%
140
18.7
2250
21.1
73%
136
20.3
69%
137
19.2
65%
138
18.2
2250
20
65%
130
18.3
62%
131
17.2
58%
131
16.3
2250
18
53%
118
14.9
50%
119
14
48%
118
13.3
2100
21.1
69%
133
19.4
65%
134
18.3
62%
135
17.4
2100
20
62%
127
17.4
59%
128
16.4
56%
128
15.6
2100
18
51%
116
14.2
48%
116
13.4
46%
116
12.7
1900
21.1
64%
128
17.8
60%
129
16.8
57%
130
15.9
1900
20
57%
122
16
54%
123
15.1
51%
123
14.3
1900
18
47%
112
13.2
44%
112
12.4
42%
111
11.8
*
Propeller RPM
**
Fuel Consumption for each Engine
Weight: 1150 kg
Pressure Altitude: 12000 ft
ISA – 30°C (-39°C)
ISA (-9°C)
ISA + 30°C (21°C)
RPM
*
MAP
PWR
KTAS
F.C.
**
PWR
KTAS
F.C.
**
PWR
KTAS
F.C.
**
[inHg]
[lt/hr]
[lt/hr]
[lt/hr]
2388
18.8
67%
135
18.8
63%
136
17.7
60%
136
16.7
2250
18.8
65%
133
18.2
61%
134
17.2
58%
134
16.3
2250
18
60%
129
16.8
57%
129
15.9
54%
129
15
2100
18.8
62%
130
17.4
59%
131
16.4
56%
132
15.5
2100
18
58%
126
16.1
54%
126
15.2
51%
126
14.4
1900
18.8
57%
125
15.9
54%
126
15
51%
126
14.2
1900
18
53%
121
14.8
50%
121
13.9
47%
121
13.2
*
Propeller RPM
**
Fuel Consumption for each Engine